• Title/Summary/Keyword: Total Pressure Recovery

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Mach 5 Performance Tests of Scramjet Engine Intake Using Free-jet Type Ground Propulsion Test Facility (자유제트형 지상추진 시험설비를 사용한 스크램제트 엔진 흡입구의 마하 5 성능시험)

  • Lee, Yang Ji;Yang, Inyoung;Lee, Kyung Jae;Oh, Jung Hwan;Choi, Jin
    • Journal of the Korean Society of Propulsion Engineers
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    • v.26 no.4
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    • pp.10-20
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    • 2022
  • The performance analysis test of the scramjet engine intake was conducted under the Mach 5 condition of the scramjet engine test facility, a free-jet ground test facility of the Korea Aerospace Research Institute. A pitot/static pressure rake installed at the rear of the isolator was designed and manufactured to measure the total pressure recovery rate and mass capture ratio, which are typical performance factors of the scramjet engine intake. The effect of the rake mounted at the rear of the isolator on the intake, the performance analysis measured by the rake, and the change in wall static pressure distribution according to the angle of attack were performed. Finally, the point at which the intake unstart occurred was confirmed by using the rear back pressure adjusting device, which simulates pressure rise in the combustor, and the results are summarized in this paper.

Enhancement of the Performance a Centrifugal Compressor in an Automobile Turbocharger by Modifying the Circumferential Inlet Height of Volute (원주방향 볼류트 입구 높이를 수정한 자동차용 터보차저 원심압축기의 성능 향상)

  • Zhou, Tianjun;Lee, Geun Sik
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.38 no.2
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    • pp.115-120
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    • 2014
  • To enhance the performance of an automobile turbocharger compressor, the circumferential inlet heights of the volute were modified and the flow field for the combined region of the diffuser and volute was numerically investigated using commercial software. Basically, a well-designed volute should have a high pressure recovery coefficient and a low loss coefficient for the total pressure. In this study, two circular volutes with the same cross sectional shape and tongue angle, but circumferentially different volute inlet heights, were selected. One volute had the middle inlet in the cross-section at the circumferential angle of $90^{\circ}$ but gradually lower inlet heights for the angles between $90^{\circ}$ to $360^{\circ}$ with respect to the cross sectional center of the volute, while maintaining the same height between the tangential line connecting the lowest positions of the cross section and the line connecting the volute inlets in the circumferential direction (case 1 volute). The other volute has an inlet height that is 2 mm lower than in case 1 volute such that the tongue section has a tangential inlet (case 2 volute). The results showed that the case 2 volute had a higher total pressure ratio because of its higher pressure recovery coefficient and higher isentropic efficiency, resulting from the lower loss coefficient along the circumferential position than the case 1 volute.

Morphological Variation and Recovery Mechanism of Residual Crude Oil by Biosurfactant from Indigenous Bacteria: Macro- and Pore-Scale Experimental Investigations

  • Song, Zhi-Yong;Han, Hong-Yan;Zhu, Wei-Yao
    • Journal of Microbiology and Biotechnology
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    • v.25 no.6
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    • pp.918-929
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    • 2015
  • Microbial enhanced oil recovery (MEOR) is being used more widely, and the biological contributions involved in MEOR need to be identified and quantified for the improvement of field applications. Owing to the excellent interfacial activity and the wide distribution of producing strains in oil reservoirs, lipopeptides have proved to be an essential part of the complex mechanisms in MEOR. In this study, crude lipopeptides were produced by a strain isolated from an indigenous community in an oil reservoir. It was found that crude lipopeptides can effectively reduce the IFT (interfacial tension) to 10-1~10-2 mN/m under high salinity without forming stable emulsions, and the wettability of natural sandstone can be enhanced (Amott index, from 0.36 to 0.48). The results of core flooding experiments indicate that an additional 5.2% of original oil in place can be recovered with a 9.5% reduction of injection pressure. After the shut-in period, the wettability of the core, the reduction of injection pressure, and the oil recovery can be improved to 0.63, 16.2% and 9.6%, respectively. In the microscopic flooding experiments, the crude oil in membrane, cluster, and throat states contribute nearly 90% in total of the additional oil recovery, and the recovery of membranestate oil was significantly enhanced by 93.3% after shut in. Based on the results in macro and pore scale, the IFT reduction and the wettability alteration are considered primary contributors to oil recovery, while the latter was more dominant after one shut-in period.

Preliminary Design Study of the Scramjet Engine Intake (스크램제트 엔진 흡입구의 기본설계 연구)

  • Kang Sang Hun;Lee Yang Ji;Yang Soo Seok
    • Journal of the Korean Society of Propulsion Engineers
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    • v.9 no.3
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    • pp.38-48
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    • 2005
  • For the development of Scramjet engine technology, intake designing processes are investigated. The basic geometry is determined by the inviuld relation such as shock wave relations and geometric relations. Furthermore, bleed duct is installed for preventing boundary layer development and shock wave impingement. Performance of the designed intake is validated by numerical analysis. As a result, double- wedge intake showed better characteristics in total pressure recovery than single-wedge intake.

Preliminary Design of Movable Ramjet Intake (가변 초음속 흡입구 기본설계)

  • Lee, Kyung-Jae;Kang, Sang-Hun;Lee, Yang-Ji;Yang, Soo-Seok
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2008.05a
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    • pp.207-210
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    • 2008
  • In this study, one type of ramjet intake were designed for the flight condition of Mach number 4 and numerical analysis was performed. In order to widen the flight envelope range (Mach number $2{\sim}6$), movable intake concept was applied. The central body was designed so that the capture area ratio which is one of most important factors of ramjet intake design could be adjusted. And various types of cowl and movable insert part of shell were designed in order to control throat area which could increase total pressure recovery. The numerical results showed that the designed ramjet intake could be applied in various flights Mach number.

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Effect of Reperfusate Solution with Latamoxef Sodium for Functional Recovery after Ischemic Cardiac Arrest in Sprague-dawley`s Isolated Heart (재관류액에 Latamoxef Sodium 첨가가 허혈성 심정지후 흰쥐 적출심장의 기능회복에 미치는 영향)

  • Ahn, B.H.;Hur, S.
    • Journal of Chest Surgery
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    • v.24 no.4
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    • pp.331-337
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    • 1991
  • Recent experimental work indicates latamoxef sodium used as a broadspectrum antibiotics generates oxygen-free radicals. The present study represents an attempt to investigate whether reperfusate containing Shiomarin[85% latamoxef sodium+15% mannitol] might decrease the post-ischemic recovery of cardiac function. In the investigation, twelve isolated rat hearts were subjected to 270 minutes of cold total global ischemia. After the cold total global ischemia, six hearts[KHB group] were reperfused with Krebs-Henseleit buffer solution and the other six hearts[LMS group] with Krebs-Henseleit buffer solution containing latamoxef sodium[200ug /L]. Postischemic recovery rate of heart rate, aortic systolic pressure, aortic flow, coronary flow and cardiac output at 20 minutes reperfusion was 100.66$\pm$10.38, 85.25$\pm$7.61, 78.95$\pm$6. 02, 78.85$\pm$8.86 and 79.11$\pm$6.54 percent respectively in the KHB group and 97.96$\pm$4.19, 87. 72$\pm$4.37, 81.74$\pm$6.80, 82.69$\pm$10.01 and 81.90$\pm$6.67 percent respectively in the LMS group. The hemodynamic data revealed no significant difference in the post-ischemic recovery rate of the two groups. This finding suggests that reperfusate containing Shiomarin[latamoxef sodium, 200ug /L] does not affect the cardiac functional recovery after cold total global ischemia.

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Effects of Induced Fatigue of Ankle Joint Muscle on the Capability and Recovery of Postural Control during Single-Leg Stance (발목 관절 근육의 유도된 피로가 외발서기 자세제어 능력과 회복에 미치는 영향)

  • Youm, Chang-Hong;Kim, Tae-Hyeon
    • Korean Journal of Applied Biomechanics
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    • v.22 no.2
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    • pp.219-228
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    • 2012
  • The purpose of this study was to investigate how induced fatigue of the ankle joint muscles affects the capability and recovery of postural control during single-leg stance in healthy adults. The study population included 22 randomly recruited men and women. Postural control was performed on single-leg stance with eyes open. Ankle joint muscle was fatigued by repeated heel raises. According to the results of this study, for the anteroposterior variables, both men and women showed significantly increased center of mass velocity and decreased center of pressure 95% edge frequency immediately after fatigue. For the mediolateral variables, both men and women showed significantly increased center of mass velocity and decreased center of pressure 95% edge frequency immediately after fatigue. For the total variables, both men and women showed significantly increased center of mass averaged-velocity immediately after fatigue, and also, the center of pressure 95% confidence ellipse area significantly increased in women. Postural control variables were not significantly different for men and women at any time (Pre, P0, P10, and P20). In conclusion, the gender does not affect the capability and recovery after induced fatigue of ankle joint muscles. The effect of fatigue found for the anteroposterior and the mediolateral variables in both men and women. Furthermore ankle joint muscle fatigue led to change of postural control strategy from an ankle joint strategy towards a hip joint strategy. These changes are believed to damage postural control. The ankle joint muscle recovered from fatigue within 20 min during single-leg stance.

Study on the Flow Characteristics of Supersonic Air Intake at Mach 4 (마하4 초음속 공기 흡입구 유동 특성에 관한 연구)

  • ;;;;Shigeru , Aso
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.34 no.10
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    • pp.61-70
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    • 2006
  • A Supersonic air intake model was designed for the high performance ramjet and dual-mode scramjet engine to operate at Mach 4 flight condition. The air intake was tested in the blowdown-type wind tunnel of Kyushu University to identify the internal flow characteristics corresponding to the flight parameters such as the back pressure, angle of attack and angle of yaw. Flow visualization was achieved by the Schlieren and oil flow visualization techniques. The intake performance was analyzed quantitatively based on the surface pressure and total Pressure measurements. The experimental results were compared with the computational fluid dynamics results. The present study exhibits the fundamental but rarely found experimental results of the high Mach number supersonic air intake.

Reconstruction of a Severely Crushed Leg with Interpositional Vessel Grafts and Latissimus Dorsi Flap

  • Park, Chan Woo;Kim, Youn Hwan;Hwang, Kyu Tae;Kim, Jeong Tae
    • Archives of Plastic Surgery
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    • v.39 no.4
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    • pp.417-421
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    • 2012
  • We present a case of a near total amputation at the distal tibial level, in which the patient emphatically wanted to save the leg. The anterior and posterior tibial nerves were intact, indicating a high possibility of sensory recovery after revascularization. The patient had open fractures at the tibia and fibula, but no bone shortening was performed. The posterior tibial vessels were reconstructed with an interposition saphenous vein graft from the contralateral side and a usable anterior tibial artery graft from the undamaged ipsilateral distal portions. The skin and soft tissue defects were covered using a subatmospheric pressure system for demarcating the wound, and a latissimus dorsi myocutaneous free flap for definite coverage of the wound. At 6 months after surgery, the patient was ambulatory without requiring additional procedures. Replantation without bone shortening, with use of vessel grafts and temporary coverage of the wound with subatmospheric pressure dressings before definite coverage, can shorten recovery time.

Numerical Simulation of a Fin-Tube Heat Exchanger for Waste Gas Heat Recovery (폐열회수용 핀-튜브 열교환기 성능 수치모사)

  • Nam, Myong-Hwan;Maeng, Jae-Hun;Koo, Byeong-Soo;Jun, Yong-Du;Lee, Kum-Bae
    • Korean Journal of Air-Conditioning and Refrigeration Engineering
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    • v.23 no.2
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    • pp.120-125
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    • 2011
  • As an effort to secure economically viable heat recovery units, innovative fin shapes for industrial boilers are studied for better performance. In the present study a numerical modeling for the analysis of heat exchanger performance is conducted using a commercial software, ANSYS CFX and the results are compared with the experimental data. Out of several candidate fin shapes curved wavy fin is selected for the present study. Both numerical and experimental data are directly compared for heat transfer rate and pressure drop with the assumed constant surface temperature of $60^{\circ}C$. Exhaust gas is obtained from a test apparatus which supplies variable flow rates. The numerical results show reasonable agreements with the experimental data within 10% in terms of both total heat transfer and pressure loss.